C 130 Hydraulic System Schematic. Main landing gear brakes 5. Web hydraulic fluid case hydraulic fluid is specially designed for high pressure applications and for the case hydraulic system.
9 C130 HYDRAULIC SYSTEM SCHEMATIC from hydraulicsawopitu.blogspot.com
Operated by engines 3, and 4. Follow all safety recommendations and safe shop practices outlined in the front of this. The type of fluid to be used depends on the.
Main Landing Gear Hydraulic Motors 3.
Wing flap hydraulic motor 2. Web hydraulic fluid case hydraulic fluid is specially designed for high pressure applications and for the case hydraulic system. Web 1 swing motor a drive isolate 2 swing brake control:
Main Landing Gear Brakes 5.
Operated by engines 3, and 4. Follow all safety recommendations and safe shop practices outlined in the front of this. Nose landing gear hydraulic system 4.
Web Utility Hydraulic System (Additional Simulated Schematic To Supplement The Main Schematic), Single Switch Type Elevator Trim Electrical Control (Control Switch And.
B swing brake solenoid valve a stabiliser. Web as you know at high altitude of aircraft less pressure is require to move rudder ( reduce pressure 1275 to 1300 psi both system) pilot must be monitored the. The type of fluid to be used depends on the.
Located On The Forward Section, Starboard Side Of The Main Landing Gear.
B axle lock a swing lock solenoid valve 53 solenoid valves (dozer/stabiliser): Web this module integrates 18 simulated electrical schematics and approximately 150 photographs and drawings to support the teaching and comprehension of this system. 2nd during flight, crew noticed an issue with the.
